How Does Angular Velocity Influence the Orientation of a Spinning Hoop?

In summary, the hoop will spin if the support is turned with a high angular velocity, and the angle between the plane of the hoop and the horizontal is approximately beta.
  • #1
FreedayFF
11
0

Homework Statement



Kleppner & Kolenkow 7.7
A thin hoop of mass M and radius R is suspended from a string
through a point on the rim of the hoop. If the support is turned with
high angular velocity [tex]\omega[/tex], the hoop will spin as shown, with its plane nearly
horizontal and its center nearly on the axis of the support. The string
makes angle [tex]\alpha[/tex] with the vertical.
Find, approximately, the small angle ([tex]\beta[/tex] between the plane of the
hoop and the horizontal.


Homework Equations





The Attempt at a Solution



torque = RMg cos[tex]\beta[/tex]
angular momentum = I[tex]\omega[/tex]

I don't know how to link these equations. I'm not really sure if this is a gyroscope problem to use its formula. Can anyone help me please?
And one question, how do I determine if a system is precessing, means it's a gyroscopic problem or not?
Thanks!
 

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  • #2
anyone please?
 
  • #3
Well, the torque on the loop (about a certain choice of origin) is just the time rate of change of the loops angular momentum (with respect to the same origin) isn't it?

So, choose an appropriate reference point (like the point where the string attaches to the support) and calculate the toque about that reference point (it is not just RMg cos[itex]\beta [/itex]) and the angular momentum of the loop avout that same reference point and then set

[itex]\mathbf{\tau}=\frac{d\textbf{L}}{dt}[/itex] and solve for [itex]\beta[/itex]...
 
  • #4
gabbagabbahey said:
Well, the torque on the loop (about a certain choice of origin) is just the time rate of change of the loops angular momentum (with respect to the same origin) isn't it?

So, choose an appropriate reference point (like the point where the string attaches to the support) and calculate the toque about that reference point (it is not just RMg cos[itex]\beta [/itex]) and the angular momentum of the loop avout that same reference point and then set

[itex]\mathbf{\tau}=\frac{d\textbf{L}}{dt}[/itex] and solve for [itex]\beta[/itex]...

how do you find torque and angular momentum of hoop about that point? the com of rope is not moving with respect to that point, so it seems that torque and angular momentum about that point is zero.
 
  • #5
FreedayFF said:

Homework Statement



Kleppner & Kolenkow 7.7
A thin hoop of mass M and radius R is suspended from a string
through a point on the rim of the hoop. If the support is turned with
high angular velocity [tex]\omega[/tex], the hoop will spin as shown, with its plane nearly
horizontal and its center nearly on the axis of the support. The string
makes angle [tex]\alpha[/tex] with the vertical.
Find, approximately, the small angle ([tex]\beta[/tex] between the plane of the
hoop and the horizontal.

Homework Equations


The Attempt at a Solution



torque = RMg cos[tex]\beta[/tex]
angular momentum = I[tex]\omega[/tex]

I don't know how to link these equations. I'm not really sure if this is a gyroscope problem to use its formula. Can anyone help me please?
And one question, how do I determine if a system is precessing, means it's a gyroscopic problem or not?
Thanks!
http://books.google.com/books?id=Hm...ough a point on the rim of the hoop"&f=false"

It says 'approximately' so i think what you're supposed to do is this.
it tells that beta is very small which is an invitation for cos(beta)=1 sin(beta)=beta

You just need to find the torque on the hoop caused by the rope (which is around the axis that goes through centre of the hoop and orthogonally to the axis of rotation and the line to rope attachment point), which is RMg, and which is equal to counter- torque caused by centrifugal force, which is an integral over the hoop.

RMg = beta*M*omega2*(integral from a=0 to a=2pi (sin(a)*R)2*da )/(2pi) =
beta*M*omega2*R2(integral from a=0 to a=2pi sin(a)2*da )/(2pi)
the indefinite integral for sin(a)2*da is 0.5*(a-sin(a)*cos(a)) + const so the definite integral is pi so that neatly simplifies out into:
RMg= beta* M*omega2*R2 / 2
g = beta* omega2*R / 2
beta = (2*g)/ omega2*R

I have neglected the distance between centre of the hoop and axis of rotation (its said to be small). I'm not sure if it is 'approximately' good enough but judging by other problems in the book, its OK.

On the second thought, it may be better to do the torque around the point where hoop is suspended, then you can easier calculate it without neglecting the distance from centre of mass and axis of rotation. I would guess though that the problem calls for neglecting that distance.

Sorry, TEX does not refresh for me when I preview, do not know why, so no tex.
 
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  • #6
Dmytry said:
http://books.google.com/books?id=Hm...ough a point on the rim of the hoop"&f=false"

It says 'approximately' so i think what you're supposed to do is this.
it tells that beta is very small which is an invitation for cos(beta)=1 sin(beta)=beta

You just need to find the torque on the hoop caused by the rope (which is around the axis that goes through centre of the hoop and orthogonally to the axis of rotation and the line to rope attachment point), which is RMg, and which is equal to counter- torque caused by centrifugal force, which is an integral over the hoop.

RMg = beta*M*omega2*(integral from a=0 to a=2pi (sin(a)*R)2*da )/(2pi) = beta*
M*omega2*R2(integral from a=0 to a=2pi sin(a)2*da )/(2pi)
the indefinite integral for sin(a)2*da is 0.5*(a-sin(a)*cos(a)) + const so the definite integral is pi so that neatly simplifies out into:
RMg= beta* M*omega2*R2 / 2
g = beta* omega2*R / 2
beta = (2*g)/ omega2*R

I have neglected the distance between centre of the hoop and axis of rotation (its said to be small). I'm not sure if it is 'approximately' good enough but judging by other problems in the book, its OK.

On the second thought, it may be better to do the torque around the point where hoop is suspended, then you can easier calculate it without neglecting the distance from centre of mass and axis of rotation. I would guess though that the problem calls for neglecting that distance.

Sorry, TEX does not refresh for me when I preview, do not know why, so no tex.

may i ask what is your education level? I'm 3rd year undergrad and these problems are very difficult for me, whereas you knocked it out with no problems.
 
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  • #7
platonic said:
may i ask what is your education level? I'm 3rd year undergrad and these problems are very difficult for me, whereas you knocked it out with no problems.
Hmm I'd recommend you to doublecheck it first, I am rusty with this (and probably there's also some way that doesn't involve the integral, i just pretty much apply brute calculus to such stuff) and I have headache.
For the precession, I didn't answer the question - I don't think there's anything complicated like that going on. The thing basically spins as a solid, around the axis, every tiny piece of mass simply spins around the axis in a horizontal circle, and all forces must balance out. It can be much more complicated if it was really dynamic, with the hoop bobbling.

Actually, just high school. But I got lucky to have PhD physics and math teachers in HS and they thought I was going to be some sort of next Feynman or something. Couldn't do that, after HS I had to move to another country and had to work for living, but got lucky to work with some PhD people. Currently living off royalties from this http://store.steampowered.com/app/67000
(shameless self promotion)
 
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  • #8
I didn't integrate anything and got the same answer as you.
I used [itex] L=L_s cos(\beta) \hat{j} + L_s sin(\beta) (-\hat{r})[/itex]
[itex]\tau=RT sin(\frac{\pi}{2} - \alpha + \beta) \hat{\theta}[/itex]
(got T from F=ma in x and y)

then used [itex]\frac{dL}{dt}=\tau[/itex]
and got [itex]\beta=\frac{2g}{R\omega^2}[/itex]

Can anyone else confirm that this is the answer ?
Thank you.
 
  • #9
[tex]\text{elementary vectors } \hat{r},\hat{\theta},\hat{k}\\
\vec{\omega} = \; <\omega \sin \beta\,,0,\omega\cos\beta\,>\\
\vec{L} = \stackrel{\leftrightarrow }{I} \vec{\omega} = \frac{MR^2}{2}\omega \sin\beta\,\hat{r} + MR^2 \omega \cos\beta\,\hat{k}\\
\text{Because for a disk, moments of inertia are: }I_\hat{k} = MR^2,\quad I_\hat{r}=\frac{MR^2}{2}\\
\\
\vec{\tau}=\frac{d}{dt}\vec{L} = \frac{MR^2}{2}\omega \sin\beta\,\dot{\hat{r}} + MR^2 \omega\cos \beta\,\dot{\hat{k}}\\
\dot{\hat{r}}= \dot{\theta}\hat{\theta}= \omega\hat{\theta} \text{ (by geometry)},\; \dot{\hat{k}}=0\\
\vec{\tau}= \frac{MR^2}{2}\omega^2\sin \beta\,\hat{\theta}\\
= RMg\cos\beta\, \hat{\theta} \quad\text{ (torque due to gravity)}\\
\text{Using small angle approximations }\sin\beta \approx \beta, \cos\beta \approx 1\text{, equating torques:}\\
\Rightarrow\beta=\frac{2g}{\omega^2R}[/tex]
 
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FAQ: How Does Angular Velocity Influence the Orientation of a Spinning Hoop?

What is a rotating hoop or gyroscope?

A rotating hoop, also known as a gyroscope, is a spinning wheel or disk that maintains its orientation regardless of any external forces acting upon it. It is often used for navigation, stabilization, and other scientific and engineering purposes.

How does a rotating hoop or gyroscope work?

A rotating hoop or gyroscope works by utilizing the principle of angular momentum. When the hoop is spinning, it creates a force perpendicular to its axis of rotation, which allows it to maintain its orientation. This force is known as gyroscopic precession.

What are some real-world applications of rotating hoop or gyroscope technology?

Rotating hoop or gyroscope technology is used in a variety of applications, including airplane and spacecraft navigation, stabilization systems for ships and submarines, and even in smartphones and other electronic devices for motion tracking and image stabilization.

What are the advantages of using a rotating hoop or gyroscope in navigation and stabilization systems?

One of the main advantages of using a rotating hoop or gyroscope is its ability to maintain its orientation even in the presence of external forces. This makes it a reliable and accurate tool for navigation and stabilization, especially in situations where other instruments may fail.

Are there any limitations or disadvantages to using a rotating hoop or gyroscope?

While rotating hoop or gyroscope technology has many advantages, it also has some limitations. For example, it can be affected by external factors such as friction and air resistance, which can cause it to lose its orientation over time. Additionally, it can be expensive and complex to design and maintain, making it less accessible for some applications.

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